LiDAR systems and methods that use a multi-facet mirror

ABSTRACT

Embodiments discussed herein refer to using LiDAR systems that uses a rotating polygon with a multi-facet mirror. Such multi-facet galvanometer mirror arrangements generate a point map that has reduced curvature.

This application is a continuation of U.S. application Ser. No.16/682,774, entitled “LIDAR SYSTEMS THAT USE A MULTI-FACET MIRROR”,filed Nov. 13, 2019, which claims the benefit of U.S. ProvisionalApplication No. 62/767,401, entitled “LIDAR SYSTEMS THAT USE AMULTI-FACET MIRROR”, filed Nov. 14, 2018. The disclosure of bothapplications are incorporated herein in their entirety. This applicationis related to U.S. application Ser. No. 16/242,534, entitled “LIDARDETECTION SYSTEMS AND METHODS,” filed on Jan. 8, 2019 and U.S.application Ser. No. 16/242,567, entitled “LIDAR DETECTION SYSTEMS ANDMETHODS THAT USE MULTI-PLANE MIRRORS,” filed on Jan. 8, 2019.

FIELD OF THE INVENTION

The present disclosure relates generally to laser scanning and, moreparticularly, to using a rotating polygon in conjunction with amulti-facet mirror.

BACKGROUND

Systems exist that enable vehicles to be driven semi-autonomously orfully autonomously. Such systems may use one or more range finding,mapping, or object detection systems to provide sensory input to assistin semi-autonomous or fully autonomous vehicle control. Light detectionand ranging (LiDAR) systems, for example, can provide the sensory inputrequired by a semi-autonomous or fully autonomous vehicle. LiDAR systemsuse light pulses to create an image or point cloud of the externalenvironment. Some typical LiDAR systems include a light source, a pulsesteering system, and light detector. The light source generates lightpulses that are directed by the pulse steering system in particulardirections when being transmitted from the LiDAR system. When atransmitted light pulse is scattered by an object, some of the scatteredlight is returned to the LiDAR system as a returned pulse. The lightdetector detects the returned pulse. Using the time it took for thereturned pulse to be detected after the light pulse was transmitted andthe speed of light, the LiDAR system can determine the distance to theobject along the path of the transmitted light pulse. The pulse steeringsystem can direct light pulses along different paths to allow the LiDARsystem to scan the surrounding environment and produce an image or pointcloud. LiDAR systems can also use techniques other than time-of-flightand scanning to measure the surrounding environment

BRIEF SUMMARY

Embodiments discussed herein refer to using LiDAR systems that use arotating polygon in conjunction with a multi-facet galvanometer mirror.Such multi-facet galvanometer mirror arrangements generate a point mapthat has reduced curvature.

In one embodiment, a LiDAR system is provided that includes a beamsteering system including a polygon having a plurality of facets andoperative to rotate around a first rotational axis, and a multi-facetmirror operative to rotate about a second rotational axis, wherein aplanar face of at least one facet of the multi-facet mirror is alignedat a non zero skew angle with respect to the second rotational axis. TheLiDAR system can also include a laser system operative to emit lightpulses that are steered by the beam steering system within a field ofview (FOV) of the LiDAR system, and a receiver system operative toprocess return pulses corresponding to the emitted light pulses togenerate a point map of the FOV.

In one embodiment, a LiDAR system is provided that includes a beamsteering system having a polygon system comprising a polygon operativeto rotate around a first rotational axis and a multi-facet mirrorsystem, which can include a mirror rotation mechanism, and a multi-facetgalvanometer mirror (MFGM) operative to rotate about a second rotationalaxis under the control of the mirror rotation mechanism, wherein theMFGM comprises a plurality of facets, and where a planar face of atleast one facet is aligned at a non zero skew angle with respect to thesecond rotational axis. The LiDAR system can include a laser systemoperative to emit a plurality of light beams that are steered by thebeam steering system within a field of view (FOV) the LiDAR system, areceiver system operative to process return pulses corresponding to theemitted light pulses to generate a point map of the FOV, and acontroller operative to control the laser system and the mirror rotationmechanism.

In one embodiment, a LiDAR system is provided that includes a beamsteering system having a motor, a polygon comprising a plurality offacets and operative to rotate around a first rotational axis, and amulti-facet mirror comprising at least two facets coupled together via ajoint member, wherein the motor is operative to oscillate a first facetof the at least two facets about a second rotational axis, and whereinthe joint member is operative to oscillate a second facet of the atleast two facets about a third rotational axis in conjunction withoperation of the motor. The LiDAR system can include a laser systemoperative to emit light pulses that are steered by the beam steeringsystem within a field of view (FOV) the LiDAR system, and a receiversystem operative to process return pulses corresponding to the emittedlight pulses to generate a point map of the FOV.

A further understanding of the nature and advantages of the embodimentsdiscussed herein may be realized by reference to the remaining portionsof the specification and the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1-3 illustrate an exemplary LiDAR system using pulse signal tomeasure distances to points in the outside environment.

FIG. 4 depicts a logical block diagram of the exemplary LiDAR system.

FIG. 5 depicts a light source of the exemplary LiDAR system.

FIG. 6 depicts a light detector of the exemplary LiDAR system.

FIG. 7 depicts an embodiment of a signal steering system using a singlelight source and detector.

FIG. 8A depicts another embodiment of a signal steering system.

FIGS. 8B-8D show simplified alternative views of the LiDAR system ofFIG. 8A according an embodiment.

FIGS. 9A-9C depict point maps from different designs.

FIG. 9D shows a point map that may be produced using LiDAR system shownin FIGS. 8B-8D according to an embodiment.

FIG. 9E shows an illustrative aperture color map produced by LiDARsystem of FIGS. 8B-8D according to an embodiment.

FIGS. 10A and 10B show simplified views of a LiDAR system according toan embodiment.

FIG. 11A shows a point map that may be produced using a LiDAR systemaccording to an embodiment.

FIG. 11B shows an illustrative aperture color map produced by a LiDARsystem, according to an embodiment.

FIGS. 12A and 12B show illustrative side and top views, respectively, ofa LiDAR system, according to an embodiment

FIG. 13 shows illustrative point map that is produced using LiDAR systemof FIGS. 12A and 12B according to an embodiment.

FIG. 14 shows illustrative point map, according to an embodiment

FIG. 15 shows a variable multi-facet galvo mirror according to anembodiment

FIG. 16A shows a point map that may be produced using a variablemulti-facet galvo mirror according to an embodiment.

FIG. 16B shows an illustrative aperture color map produced by a LiDARsystem using a variable multi-facet galvo mirror, according to anembodiment.

FIG. 17 shows an illustrative LiDAR system according to an embodiment.

FIG. 18 shows an illustrative block diagram of a LiDAR system accordingto an embodiment.

FIG. 19 shows illustrative field of view of a LiDAR system according toan embodiment.

FIGS. 20A and 20B shows an illustrative multi-facet mirror arrangementbeing used in LiDAR system 2000 according to an embodiment.

FIGS. 21A and 21B show respective point map and aperture color map.

DETAILED DESCRIPTION

Illustrative embodiments are now described more fully hereinafter withreference to the accompanying drawings, in which representative examplesare shown. Indeed, the disclosed LiDAR systems and methods may beembodied in many different forms and should not be construed as limitedto the embodiments set forth herein. Like numbers refer to like elementsthroughout.

In the following detailed description, for purposes of explanation,numerous specific details are set forth to provide a thoroughunderstanding of the various embodiments. Those of ordinary skill in theart will realize that these various embodiments are illustrative onlyand are not intended to be limiting in any way. Other embodiments willreadily suggest themselves to such skilled persons having the benefit ofthis disclosure.

In addition, for clarity purposes, not all of the routine features ofthe embodiments described herein are shown or described. One of ordinaryskill in the art would readily appreciate that in the development of anysuch actual embodiment, numerous embodiment-specific decisions may berequired to achieve specific design objectives. These design objectiveswill vary from one embodiment to another and from one developer toanother. Moreover, it will be appreciated that such a development effortmight be complex and time-consuming but would nevertheless be a routineengineering undertaking for those of ordinary skill in the art havingthe benefit of this disclosure.

Some light detection and ranging (LiDAR) systems use a single lightsource to produce one or more light signals of a single wavelength thatscan the surrounding environment. The signals are scanned using steeringsystems that direct the pulses in one or two dimensions to cover an areaof the surrounding environment (the scan area). When these systems usemechanical means to direct the pulses, the system complexity increasesbecause more moving parts are required. Additionally, only a singlesignal can be emitted at any one time because two or more identicalsignals would introduce ambiguity in returned signals. In someembodiments of the present technology, these disadvantages and/or othersare overcome.

For example, some embodiments of the present technology use one or morelight sources that produce light signals of different wavelengths and/oralong different optical paths. These light sources provide the signalsto a signal steering system at different angles so that the scan areasfor the light signals are different (e.g., if two light sources are usedto create two light signals, the scan area associated with each lightsource is different). This allows for tuning the signals to appropriatetransmit powers and the possibility of having overlapping scan areasthat cover scans of different distances. In addition, overlappingscanning areas enable regions of higher resolution. Longer ranges can bescanned with signals having higher power and/or slower repetition rate(e.g., when using pulsed light signals). Shorter ranges can be scannedwith signals having lower power and/or high repetition rate (e.g., whenusing pulse light signals) to increase point density.

As another example, some embodiments of the present technology usesignal steering systems with one or more dispersion elements (e.g.,gratings, optical combs, prisms, etc.) to direct pulse signals based onthe wavelength of the pulse. A dispersion element can make fineadjustments to a pulse's optical path, which may be difficult orimpossible with mechanical systems. Additionally, using one or moredispersion elements allows the signal steering system to use fewmechanical components to achieve the desired scanning capabilities. Thisresults in a simpler, more efficient (e.g., lower power) design that ispotentially more reliable (due to few moving components).

Some LiDAR systems use the time-of-flight of light signals (e.g., lightpulses) to determine the distance to objects in the path of the light.For example, with respect to FIG. 1 , an exemplary LiDAR system 100includes a laser light source (e.g., a fiber laser), a steering system(e.g., a system of one or more moving mirrors), and a light detector(e.g., a photon detector with one or more optics). LiDAR system 100transmits light pulse 102 along path 104 as determined by the steeringsystem of LiDAR system 100. In the depicted example, light pulse 102,which is generated by the laser light source, is a short pulse of laserlight. Further, the signal steering system of the LiDAR system 100 is apulse signal steering system. However, it should be appreciated thatLiDAR systems can operate by generating, transmitting, and detectinglight signals that are not pulsed can be used to derive ranges to objectin the surrounding environment using techniques other thantime-of-flight. For example, some LiDAR systems use frequency modulatedcontinuous waves (i.e., “FMCW”). It should be further appreciated thatany of the techniques described herein with respect to time-of-flightbased systems that use pulses also may be applicable to LiDAR systemsthat do not use one or both of these techniques.

Referring back to FIG. 1 (a time-of-flight LiDAR system that uses lightpulses) when light pulse 102 reaches object 106, light pulse 102scatters and returned light pulse 108 will be reflected back to system100 along path 110. The time from when transmitted light pulse 102leaves LiDAR system 100 to when returned light pulse 108 arrives back atLiDAR system 100 can be measured (e.g., by a processor or otherelectronics within the LiDAR system). This time-of-flight combined withthe knowledge of the speed of light can be used to determine therange/distance from LiDAR system 100 to the point on object 106 wherelight pulse 102 scattered.

By directing many light pulses, as depicted in FIG. 2 , LiDAR system 100scans the external environment (e.g., by directing light pulses 102,202, 206, 210 along paths 104, 204, 208, 212, respectively). As depictedin FIG. 3 , LiDAR system 100 receives returned light pulses 108, 302,306 (which correspond to transmitted light pulses 102, 202, 210,respectively) back after objects 106 and 214 scatter the transmittedlight pulses and reflect pulses back along paths 110, 304, 308,respectively. Based on the direction of the transmitted light pulses (asdetermined by LiDAR system 100) as well as the calculated range fromLiDAR system 100 to the points on objects that scatter the light pulses(e.g., the points on objects 106 and 214), the surroundings within thedetection range (e.g., the field of view between path 104 and 212,inclusively) can be precisely plotted (e.g., a point cloud or image canbe created).

If a corresponding light pulse is not received for a particulartransmitted light pulse, then it can be determined that there are noobjects that can scatter sufficient amount of signal for the LiDAR lightpulse within a certain range of LiDAR system 100 (e.g., the max scanningdistance of LiDAR system 100). For example, in FIG. 2 , light pulse 206will not have a corresponding returned light pulse (as depicted in FIG.3 ) because it did not produce a scattering event along its transmissionpath 208 within the predetermined detection range. LiDAR system 100 (oran external system communication with LiDAR system 100) can interpretthis as no object being along path 208 within the detection range ofLiDAR system 100.

In FIG. 2 , transmitted light pulses 102, 202, 206, 210 can betransmitted in any order, serially, in parallel, or based on othertimings with respect to each other. Additionally, while FIG. 2 depicts a1-dimensional array of transmitted light pulses, LiDAR system 100optionally also directs similar arrays of transmitted light pulses alongother planes so that a 2-dimensional array of light pulses istransmitted. This 2-dimensional array can be transmitted point-by-point,line-by-line, all at once, or in some other manner. The point cloud orimage from a 1-dimensional array (e.g., a single horizontal line) willproduce 2-dimensional information (e.g., (1) the horizontal transmissiondirection and (2) the range to objects). The point cloud or image from a2-dimensional array will have 3-dimensional information (e.g., (1) thehorizontal transmission direction, (2) the vertical transmissiondirection, and (3) the range to objects).

The density of points in point cloud or image from a LiDAR system 100 isequal to the number of pulses divided by the field of view. Given thatthe field of view is fixed, to increase the density of points generatedby one set of transmission-receiving optics, the LiDAR system shouldfire a pulse more frequently, in other words, a light source with ahigher repetition rate is needed. However, by sending pulses morefrequently the farthest distance that the LiDAR system can detect may bemore limited. For example, if a returned signal from a far object isreceived after the system transmits the next pulse, the return signalsmay be detected in a different order than the order in which thecorresponding signals are transmitted and get mixed up if the systemcannot correctly correlate the returned signals with the transmittedsignals. To illustrate, consider an exemplary LiDAR system that cantransmit laser pulses with a repetition rate between 500 kHz and 1 MHz.Based on the time it takes for a pulse to return to the LiDAR system andto avoid mix-up of returned pulses from consecutive pulses inconventional LiDAR design, the farthest distance the LiDAR system candetect may be 300 meters and 150 meters for 500 kHz and 1 Mhz,respectively. The density of points of a LiDAR system with 500 kHzrepetition rate is half of that with 1 MHz. Thus, this exampledemonstrates that, if the system cannot correctly correlate returnedsignals that arrive out of order, increasing the repetition rate from500 kHz to 1 Mhz (and thus improving the density of points of thesystem) would significantly reduce the detection range of the system.

FIG. 4 depicts a logical block diagram of LiDAR system 100, whichincludes light source 402, signal steering system 404, pulse detector406, and controller 408. These components are coupled together usingcommunications paths 410, 412, 414, 416, and 418. These communicationspaths represent communication (bidirectional or unidirectional) amongthe various LiDAR system components but need not be physical componentsthemselves. While the communications paths can be implemented by one ormore electrical wires, busses, or optical fibers, the communicationpaths can also be wireless channels or open-air optical paths so that nophysical communication medium is present. For example, in one exemplaryLiDAR system, communication path 410 is one or more optical fibers,communication path 412 represents an optical path, and communicationpaths 414, 416, 418, and 420 are all one or more electrical wires thatcarry electrical signals. The communications paths can also include morethan one of the above types of communication mediums (e.g., they caninclude an optical fiber and an optical path or one or more opticalfibers and one or more electrical wires).

LiDAR system 100 can also include other components not depicted in FIG.4 , such as power buses, power supplies, LED indicators, switches, etc.Additionally, other connections among components may be present, such asa direct connection between light source 402 and light detector 406 sothat light detector 406 can accurately measure the time from when lightsource 402 transmits a light pulse until light detector 406 detects areturned light pulse.

FIG. 5 depicts a logical block diagram of one example of light source402 that is based on a fiber laser, although any number of light sourceswith varying architecture could be used as part of the LiDAR system.Light source 402 uses seed 502 to generate initial light pulses of oneor more wavelengths (e.g., 1550 nm), which are provided towavelength-division multiplexor (WDM) 504 via fiber 503. Pump 506 alsoprovides laser power (of a different wavelength, such as 980 nm) to WDM504 via fiber 505. The output of WDM 504 is provided to pre-amplifiers508 (which includes one or more amplifiers) which provides its output tocombiner 510 via fiber 509. Combiner 510 also takes laser power frompump 512 via fiber 511 and provides pulses via fiber 513 to boosteramplifier 514, which produces output light pulses on fiber 410. Theoutputted light pulses are then fed to steering system 404. In somevariations, light source 402 can produce pulses of different amplitudesbased on the fiber gain profile of the fiber used in the source.Communication path 416 couples light source 402 to controller 408 (FIG.4 ) so that components of light source 402 can be controlled by orotherwise communicate with controller 408. Alternatively, light source402 may include its own controller. Instead of controller 408communicating directly with components of light source 402, a dedicatedlight source controller communicates with controller 408 and controlsand/or communicates with the components of light source 402. Lightsource 402 also includes other components not shown, such as one or morepower connectors, power supplies, and/or power lines.

Some other light sources include one or more laser diodes, short-cavityfiber lasers, solid-state lasers, and/or tunable external cavity diodelasers, configured to generate one or more light signals at variouswavelengths. In some examples, light sources use amplifiers (e.g.,pre-amps or booster amps) include a doped optical fiber amplifier, asolid-state bulk amplifier, and/or a semiconductor optical amplifier,configured to receive and amplify light signals.

Returning to FIG. 4 , signal steering system 404 includes any number ofcomponents for steering light signals generated by light source 402. Insome examples, signal steering system 404 may include one or moreoptical redirection elements (e.g., mirrors or lens) that steer lightpulses (e.g., by rotating, vibrating, or directing) along a transmitpath to scan the external environment. For example, these opticalredirection elements may include MEMS mirrors, rotating polyhedronmirrors, or stationary mirrors to steer the transmitted pulse signals todifferent directions. Signal steering system 404 optionally alsoincludes other optical components, such as dispersion optics (e.g.,diffuser lenses, prisms, or gratings) to further expand the coverage ofthe transmitted signal in order to increase the LiDAR system 100'stransmission area (i.e., field of view). An example signal steeringsystem is described in U.S. Patent Application Publication No.2018/0188355, entitled “2D Scanning High Precision LiDAR UsingCombination of Rotating Concave Mirror and Beam Steering Devices,” thecontent of which is incorporated by reference in its entirety herein forall purposes. In some examples, signal steering system 404 does notcontain any active optical components (e.g., it does not contain anyamplifiers). In some other examples, one or more of the components fromlight source 402, such as a booster amplifier, may be included in signalsteering system 404. In some instances, signal steering system 404 canbe considered a LiDAR head or LiDAR scanner.

Some implementations of signal steering systems include one or moreoptical redirection elements (e.g., mirrors or lens) that steersreturned light signals (e.g., by rotating, vibrating, or directing)along a receive path to direct the returned light signals to the lightdetector. The optical redirection elements that direct light signalsalong the transmit and receive paths may be the same components (e.g.,shared), separate components (e.g., dedicated), and/or a combination ofshared and separate components. This means that in some cases thetransmit and receive paths are different although they may partiallyoverlap (or in some cases, substantially overlap).

FIG. 6 depicts a logical block diagram of one possible arrangement ofcomponents in light detector 404 of LiDAR system 100 (FIG. 4 ). Lightdetector 404 includes optics 604 (e.g., a system of one or more opticallenses) and detector 602 (e.g., a charge coupled device (CCD), aphotodiode, an avalanche photodiode, a photomultiplier vacuum tube, animage sensor, etc.) that is connected to controller 408 (FIG. 4 ) viacommunication path 418. The optics 604 may include one or more photolenses to receive, focus, and direct the returned signals. Lightdetector 404 can include filters to selectively pass light of certainwavelengths. Light detector 404 can also include a timing circuit thatmeasures the time from when a pulse is transmitted to when acorresponding returned pulse is detected. This data can then betransmitted to controller 408 (FIG. 4 ) or to other devices viacommunication line 418. Light detector 404 can also receive informationabout when light source 402 transmitted a light pulse via communicationline 418 or other communications lines that are not shown (e.g., anoptical fiber from light source 402 that samples transmitted lightpulses). Alternatively, light detector 404 can provide signals viacommunication line 418 that indicate when returned light pulses aredetected. Other pulse data, such as power, pulse shape, and/orwavelength, can also be communicated.

Returning to FIG. 4 , controller 408 contains components for the controlof LiDAR system 100 and communication with external devices that use thesystem. For example, controller 408 optionally includes one or moreprocessors, memories, communication interfaces, sensors, storagedevices, clocks, ASICs, FPGAs, and/or other devices that control lightsource 402, signal steering system 404, and/or light detector 406. Insome examples, controller 408 controls the power, rate, timing, and/orother properties of light signals generated by light source 402;controls the speed, transmit direction, and/or other parameters of lightsteering system 404; and/or controls the sensitivity and/or otherparameters of light detector 406.

Controller 408 optionally is also configured to process data receivedfrom these components. In some examples, controller determines the timeit takes from transmitting a light pulse until a corresponding returnedlight pulse is received; determines when a returned light pulse is notreceived for a transmitted light pulse; determines the transmitteddirection (e.g., horizontal and/or vertical information) for atransmitted/returned light pulse; determines the estimated range in aparticular direction; and/or determines any other type of data relevantto LiDAR system 100.

FIG. 7 depicts an embodiment of a signal steering system (e.g., signalsteering system 404 of FIG. 4 ) according to some embodiments of thepresent technology. Polygon 702 has ten reflective sides (sides702A-702E are visible in FIG. 7 ) but can have any number of reflectivesides. For example, other examples of polygon 702 has 6, 8, or 20sides). Polygon 702 rotates about axis 703 based on a drive motor (notshown) to scan signals delivered from a light source (e.g., via output706, which is connected to a light source such as light source 402described above) along a direction perpendicular or at a non-zero angleto axis of rotation 703.

Mirror galvanometer 704 is positioned next to polygon 702 so that one ormore signals emitted from light source output 706 (e.g., a fiber tip)reflect off of mirror galvanometer 704 and onto rotating polygon 702.Mirror galvanometer 704 tilts so as to scan one or more signals fromoutput 706 to a direction different than the direction that polygon 702scans signals In some examples, polygon 702 is responsible for scanningone or more signals in the horizontal direction of the LiDAR system andmirror galvanometer 704 is responsible for scanning one or more signalsin the vertical direction. In some other examples, polygon 702 andmirror galvanometer 704 are configured in the reverse manner. While theexample in FIG. 7 uses a mirror galvanometer, other components can beused in its place. For example, one or more rotating mirrors or agrating (with different wavelength pulses) may be used. The solid blackline represents one example signal path through the signal steeringsystem.

Light returned from signal scattering (e.g., when a light hits anobject) within region 708 (indicated by dashed lines) is returned torotating polygon 702, reflected back to mirror galvanometer 704, andfocused by lens 710 onto detector 712. While lens 710 is depicted as asingle lens, in some variations it is a system of one or more optics.

FIG. 8A depicts a similar system as depicted in FIG. 7 except a secondlight source is added that provides one or more signals from output 714.The light source for output 714 may be the same or different than thelight source for output 706, and the light transmitted by output 714 mayhave the same or a different wavelength as the light transmitted byoutput 706. Using multiple light outputs can increase the points densityof a points map without sacrificing the maximum unambiguous detectionrange of the system. For example, light output 714 can be positioned totransmit light at a different angle from output 706. Because of thedifferent angles, light transmitted from light source 706 is directed toan area different from light transmitted from output 714. The dottedline shows one example pulse path for pulses emitted from output 714.Consequently, one or more objects located at two different areas withina region can scatter and return light to the LiDAR system. For example,the region 716 (the dashed/double-dotted line) indicates the region fromwhich return signals from scattered signals returns to the LiDAR system.The returned light is reflected off polygon 702 and mirror galvanometer704 and focused on detectors 712 and 718 by lens 710. Detectors 712 and718 can each be configured to receive returned light from one of theoutputs 706 and 714, and such configuration can be achieved by preciselycontrolling the position of the detectors 712 and 718 as well as thewavelength(s) of the transmitted light. Note that the same lens (oroptic system) can be used for both detector 712 and 718. The offsetbetween outputs 706 and 714 means that the light returned to the LiDARsystem will have a similar offset. By properly positioning detectors 712and 718 based on the relative positioning of their respective lightsource outputs (e.g., respective positions of outputs 706 and 714) and,optionally, by properly controlling the wavelength(s) of the transmittedlight, the returned light will be properly focused on to the correctdetectors, and each received light can be a point in the points map.Each received light pulse can be interpreted as a point in 3D space.Therefore, compared to the system with only one output 706, the systemwith two outputs can maintain the same pulse repetition rate and producetwice the number of points or reduce the pulse repetition rate by halfand still produce the same number of points. As a non-limiting example,a system with two light outputs can reduce the pulse repetition ratefrom 1 MHz to 500 KHz, thereby increasing its maximum unambiguousdetection range from 150 meters to 300 meters, without sacrificingpoints density of the resulting points map. A pulse repetition rate ofbetween 200 kHz and 2 MHz is contemplated and disclosed.

FIGS. 8B-8D show simplified alternative views of the LiDAR system ofFIG. 8A according an embodiment. In particular, FIGS. 8B and 8C showillustrative top views and FIG. 8D shows an illustrative side view. Asshown, polygon 810 has six facets 811-816 and mirror galvanometer 820has one facet. Mirror 820 rotates about mirror rotation axis 825. Mirror820 is aligned such that is parallel to rotation axis 825. That is, aplanar face of mirror 820 is parallel to the mirror rotation axis 825. Askew angle is defined as the angle existing between the planar face ofthe mirror and the rotation axis. When the planar face and the rotationaxis are parallel to each other, the skew angle is zero (0). Two lightbeams 830 and 832 are shown originating from their respective sources(not shown) by first interfacing with mirror galvanometer 820 and theninterfacing with polygon 810, which redirects the light beams to theFOV. Depending on the rotation orientation of polygon 810, light beams830 and 832 may interact with the same facet (as shown in FIG. 8C) ortwo or more facets (as shown in FIG. 8B). Simultaneous interaction withmultiple facets can increase the field of view of the LiDAR system,however, the point maps obtained from such a polygon/galvanometer mirrorconfiguration may include curvature such as that shown, for example, inFIGS. 9A-9D, below.

FIG. 9A depicts a point map from a first design. This design has twochannels (e.g., two light source outputs and two light detectors) placedin a way that the exiting beams have an angle of 8 degrees between them.The scanned pattern has vertical overlap. The scanned range is +−56degrees horizontally and +12˜−20 degrees vertically.

FIG. 9B depicts a point map from a second design. This design has twochannels (e.g., two light source outputs and two light detectors) placedin a way that the exiting beams have an angle of 6 degrees between them.The scanned pattern has horizontal overlap (+−45 degrees). The scannedrange is +−67 degrees horizontally and +12˜−20 degrees vertically.

Exiting beams of two channels are not necessary to separate with acertain angle (e.g. 6 degree in FIG. 9B) to obtain a larger horizontalrange. Horizontal displacement of existing beams can be used to expandthe horizontal range. For example, two exit beams may be pointed thatsame angle, but are offset with respect to each other in the same plane.Due to these different positions, each channel is reflected by differentpart of polygon and therefore covers a different horizontal range. Bycombining the two channels, the total horizontal range is increased.

FIG. 9C depicts a point map from a third design. This design has threechannels (e.g., three light source outputs and three light detectors) toincrease point density. About 2.88 million points per second can beobtained by using 3 fiber tips and 3 detectors. The resolution can befurther reduced to 0.07 degrees for both directions. The speed of thepolygon can be reduced to 6000 rpm.

FIG. 9D shows a point map that may be produced using LiDAR system shownin FIGS. 8B-8D according to an embodiment. As shown, the point map showsthat a relatively large FOV is captured (e.g., approximately −100 to+100 degrees), with curvature being present. FIG. 9E shows anillustrative aperture color map produced by LiDAR system of FIGS. 8B-8D.The aperture refers to the area, or cross section, of the receivingoptics and is proportional to the transmitted light energy that isreceived and detected.

FIGS. 10A and 10B show simplified views of LiDAR system 1000 accordingto an embodiment. LiDAR system 1000 includes polygon 1010, whichincludes facets 1011-1016, and single faceted mirror 1020. Mirror 1020is sized such that it is able to reflect light beams that simultaneouslyinteract with three different facets of polygon 1010 (as shown in FIG.10B). Mirror 1020 rotates about mirror rotation axis 1025. Mirror 1020is aligned such that its planar surface is parallel to rotation axis1025, resulting in a skew angle of 0. Three laser beams 1031-1033 areshown interfacing with mirror 1020, which redirects beams 1031-1033 tofacets 1011-1013, respectively.

FIG. 11A shows a point map that may be produced using LiDAR system 1000according to an embodiment. As shown, the point map shows that arelatively large FOV is captured (e.g., approximately −140 to +140degrees), but substantial curvature is present. FIG. 11B shows anillustrative aperture color map produced by LiDAR system 1000.

Embodiments discussed herein use a multi-faceted mirror to produce amore desirable point map profile. Characteristics of a more desirablepoint map include point maps that are not excessively bowed and exhibitrelatively flat profiles. In some embodiments, a desirable point map mayexhibit a rectangular or square shape. It is also desirable to produce apoint map that captures a wide field of view, for example, in thehorizontal left-to-right or right-to-left orientation.

FIGS. 12A and 12B show illustrative side and top views, respectively, ofLiDAR system 1200, according to an embodiment. Lidar system 1200 caninclude multi-faceted polygon 1210 that spins about rotation axis 1215and multi-faceted galvanometer mirror 1220. Four light beams 1231-1234are shown interacting with multi-faceted galvanometer mirror 1220 andpolygon 1210. Multi-faceted galvanometer mirror 1220 pivots about singlerotation axis 1225. Multi-faceted galvanometer mirror 1220 is shown toinclude two facets 1221 and 1222, though it should be understood thatthree or more facets may be used. Facets 1221 and 1222 may be coupled toa common structure (not shown) that is coupled to a moving member (e.g.,motor) so that when the moving member changes position of the commonstructure, facets 1221 and 1222 both move in unison. Facets 1221 and1222 are positioned side by side (as shown in FIG. 12B) with a fixeddistance between them (as shown) or facets 1221 and 1222 can be indirect contact with each. In addition, facets 1221 and 1222 are arrangedsuch that their respective faces are not parallel to each other, andsuch that they are not parallel with mirror rotation axis 1225. In otherwords, skew angle, α, exists between the planar face of each of facets1221 and 1222 and mirror rotation axis 1225, where α is not equal to 0degrees. In some embodiments, the angle, α, may be fixed as an acuteangle or an obtuse angle. In other embodiments, the angle, α, may bevariable thereby enabling facets 1221 and 1222 to move relative to eachother. In this variable angle embodiment, facets 1221 and 1222 may move,for example, in a butterfly fashion. Variable angle embodiments arediscussed in more detail below.

Producing a more desirable point map using a multi-facet galvanometermirror may take many different considerations into account.Considerations pertaining to polygon 1210 are discussed first. Polygon1210 can be designed to have any number of facets. The construction andorientation of each facet may be such that an angle of polygon facetswith respect to rotation axis 1215 is set to a particular angle, shownas g. Polygon 1210 spins about rotation axis 1215 at one or morepredetermined speeds. A tilt angle, shown as b, may exist betweenrotation axis 1215 and a vertical (gravity) axis.

Considerations pertaining to mirror 1220 are now discussed. The locationof mirror rotation axis 1225 with respect to polygon 1210 is a factor.The positioning of facets 1221 and 1222 with respect to polygon 1210 isa factor. For example, in FIG. 12B, facets 1221 and 1222 are centeredwith respect to the 0 degree angle along the Y axis. If desired, facets1221 and 1222 can be repositioned to be biased to the left or right sideof the FOV. The skew angle, which is the angle of facets 1221 and 1222with respect to mirror rotation axis 1225, is another factor that can bemanipulated. In a “normal” case, where a single facet mirror is parallelto the rotation axis, skew angle is 0. As shown in FIG. 12B, facets 1221and 1222 are not parallel to mirror rotation axis 1225 and thus haveaskew angle that is nonzero.

Yet other factors that affect the point map include the number of laserbeams being used. This includes beam angle and launch point of eachlaser beam. In some embodiments, the laser beams may be symmetricallydistributed across mirror 1220. For example, if there are four beams,two beams may be projected to facet 1221 and two beams may be projectedto facet 1222. In other embodiments, the laser beams may beasymmetrically distributed across 1220. For example, if there are fourbeams, three beams may be projected on to facet 1221 and one beam may beprojected on facet 1222. Any one or more of the above considerations canbe modified to produce a desired point map.

FIG. 13 shows illustrative point map 1300 that is produced using LiDARsystem 1200 according to an embodiment. FIG. 13 shows illustrative beamangle and launch points, the tilt angle, b, the angle of facet, g,position of the galvo mirror rotation axis shown by Xm and Ym, and theskew angle. FIG. 14 shows illustrative point map 1400 that is producedusing LiDAR system 1200 according to an embodiment. Point map 1400 isproduced using a different tilt angle, b, than the tilt angle being usedto produce point map 1300.

FIG. 15 shows a variable multi-facet galvo mirror 1500 according to anembodiment. In particular, FIG. 15 shows that the skew angle changeswith time. In particular, at time, t₁, the skew angle is equal to x,then at time, t₂, the skew angle is equal to y, and at time, t₃, theskew angle is equal to z, where x>y>z. Both facets of mirror 1500 rotatealong mirror rotation axis 1505, but the skew angle is variable. In someembodiments, the skew angle can be controlled independent of therotation angle of mirror 1500 along its rotation axis 1505. In someembodiments, the skew angle can be linearly dependent on the rotationangle of mirror 1500 along mirror rotation axis 1505. For example, theskew angle can be set to A+/−(C*ϕ), where A is a skew angle constant, Cis a multiplication factor, and ϕ is the mirror rotation angle of thegalvo mirror axis.

Although not shown in FIG. 15 , it should be appreciated that the skewangle can change from a positive skew angle to a negative skew angle, orvice versa (and pass through a zero skew angle). It should also beappreciated that each facet may be independently controlled to have toits own controlled skew angle. For example, of the two facets shown inFIG. 15 , the skew angle of one facet can be changed independently ofthe skew angle of the other facet. A benefit of the independent controlof the skew angle of each facet is that it may enable dynamic controlover the point map.

FIG. 16A shows a point map that may be produced using variablemulti-facet galvo mirror 1500 according to an embodiment. As shown, thepoint map shows that a relatively rectangular FOV is captured. FIG. 16Bshows an illustrative aperture color map produced by a LiDAR systemusing variable multi-facet galvo mirror 1500. FIG. 16B shows that twoseparate relatively high intensity apertures exist at about −40 degreesand at +40 degrees in the horizontal angle.

FIG. 17 shows illustrative LiDAR system 1700 according to an embodiment.System 1700 includes polygon 1710 and three facet mirror 1720 thatrotates about rotation axis 1725. Three facet mirror 1720 includesfacets 1721-1723. Facet 1722 is parallel with rotation axis 1725 andthus has a zero skew angle. Facets 1721 and 1723 are not parallel withrotation axis 1725 and have respective skew angles of α₁ and α₂. In oneembodiment, skew angles α₁ and α₂ may be fixed. In another embodiment,skew angles α₁ and α₂ may be variable. As a specific example, thevariability of skew angles α₁ and α₂ can be jointly controlled such thatα₁ is always equal to α₂. As another specific example, skew angles α₁and α₂ can be independently controlled such that α₁ is not necessary thesame as α₂.

FIG. 18 shows an illustrative block diagram of LiDAR system 1800according to an embodiment. LiDAR system 1800 can include lasersubsystem 1810, receiver system 1820, beam steering system 1830, andcontroller 1860. Laser subsystem 1810 can include laser source 1812 andbeam angle controller 1814. Receiver system 1820 can include optics,detectors, and other components (all which are not shown). Beam steeringsystem 1830 can include multi-facet mirror system 1840 and polygonsystem 1850. Mirror system 1840 can include multi-facet mirror 1842,mirror rotation mechanism 1844, and skew angle control mechanism 1846.Polygon system 1850 can include polygon 1852 and rotation axis control1854. Controller 1860 may include repetition rate module 1862, range ofinterest (ROI) module 1864, skew angle module 1866, beam angle module1868, multi-facet mirror (MFM) control module 1870, and rotation axistilt module 1872. LiDAR system 1800 may be contained within one or morehousings. In multiple housing embodiments, at least one of the housingsmay be a temperature controlled environment in which select portions ofLiDAR system 1800 (e.g., laser source 1812 and controller 1860) arecontained therein.

Laser subsystem 1810 may include laser source 1812 and beam anglecontroller 1814. Laser subsystem 1810 is operative to direct lightenergy towards beam steering system 1830, which directs light energy toa FOV of the LiDAR system. Laser source 1812 may serve as the onlysource of light energy, but the light energy may be split into N numberof beams using any suitable beam splitting technique or mechanism. Eachbeam may be positioned within system 1800 to have a particular beamangle and a particular launch point. The beam angle and launch point mayaffect the point map generated when used in conjunction with beamsteering system 1830. In some embodiments, the beam angle and launchpoint may be fixed. In other embodiments, the beam angle and/or launchpoint for each beam may be variable and can be controlled by beam anglecontroller 1814. For example, beam angle controller 1814 may be able toadjust an angle of one or more of the beams based on inputs provided bybeam angle module 1868 in controller 1860.

Laser source 1812 may be operative to control the repetition rate atwhich light energy is emitted in response to controls provided byrepetition rate module 1862. The repetition rate refers to the rate atwhich successive light pulses are emitted by laser source 1812. In someembodiments, the repetition rate may remain fixed. In other embodiments,the repetition rate may be varied. Variation in the repetition rate maybe based on a number of different factors, including, for example,desired point map resolution or one or more regions of interest withinthe FOV, multi-facet mirror movement speed, polygon movement speed, tiltaxis, skew angle, and any other suitable criteria. The multi-facetmirror movement speed may refer to the rotation speed of multi-facetmirror 1842. The polygon movement speed may refer to the rotation speedof polygon 1850. Tilt axis may refer to the difference between therotation axis of polygon 1850 with respect to a gravitational axis.

Multi-facet mirror 1842 may move under the direction of mirror rotationmechanism 1844 and optionally further under control of skew anglecontrol mechanism 1846. Multi-facet mirror 1842 is operative to redirectlight beams originating from laser source 1812 to polygon 1852. Inaddition, multi-facet mirror 1842 is operative to redirect return pulsesreceived via polygon 1852 to receiver system 1820. In one embodiment,mirror rotation mechanism 1844 may be a motor that is coupled tomulti-facet mirror 1842. Multi-facet mirror 1842 may be rotated aboutits rotation axis under the control of MFM control 1870. In embodimentswhere the skew angle of multi-facet mirror 1842 is fixed, skew anglecontrol mechanism 1846 is not used. In embodiments where the skew angleof multi-facet mirror 1842 is variable, skew angle control mechanism1846 may be used. Skew angle module 1866 may control the skew angle byinstructing skew angle control mechanism 1846. Skew angle controlmechanism 1846 may control the skew angle independent of the rotation ordependent on the rotation of multi-facet mirror 1842. If multi-facetmirror 1842 has multiple skew angles, skew angle control mechanism 1846may exercise independent control over each skew angle. Skew anglecontrol mechanism 1846 may use mechanical linkages to control theposition of the skew angle. For example, the mechanical linkage can be ascrew based linkage, rack and pinion linkage, or ball screw linkage. Insome embodiments, the linkage can be directly tied to mirror rotationmechanism 1844 such that the skew angle is dependent on the rotationposition of the mirror along its rotation axis.

Polygon 1852 rotates under the control of rotation axis control 1854 andis operative to direct the light energy received from mirror 1842 to theFOV of LiDAR system 1800. Rotation axis control 1854 may control thespeed at which polygon 1852 rotates under the control of MFM controlmodule 1870. Rotation axis control 1854 may also adjust a tilt angle ofpolygon 1852 under the control of MFM control module 1870.

Controller 1860 is operative to control operation of LiDAR system 1800.Controller 1860 can control where within the FOV light pulses aredirected and can process return pulses to populate a point map that maybe used by another system such as, for example, an autonomous car. Themodules (e.g., modules 1862, 1864, 1866, 1868, 1870, and 1872) may beresponsible for controlling the point maps generated using system 1800.Some modules may be interdependent on each other whereas other modulesmay operate independent of others. The modules may incorporate real-timefeedback of point map performance to make necessary adjustments to, forexample, repetition rate, mirror rotations speed, skew angle, tilt, etc.The modules may operate based on different modes of operation. Forexample, LiDAR system 1800 may receive an external input such as vehiclespeed, which may be used to determine which mode LiDAR system 1800should operate. In a first vehicle speed mode (e.g., a slow speed mode),the modules may configure LiDAR system 1800 to operate accordingly toproduce point maps more suitable for the first mode. In a second vehiclespeed mode, (e.g., a fast speed mode), the modules may configure LiDARsystem 1800 to operate accordingly to produce point maps more suitablefor the second mode.

Repetition rate module 1862 may control the repetition rate or timeinterval of successive light beam emissions of laser source 1812. Therepetition rate may be coordinated with one or more of regions ofinterest, skew angle, mirror rotation speed, and rotation axis tilt. ROImodule 1864 may be responsible for controlling laser subsystem 1810 andbeam steering system 1830 to ensure one or more regions of interestwithin the FOV are more accurately captured in the point map. FIG. 19shows illustrative field of view (FOV) 1900 of a LiDAR system accordingto an embodiment. As shown, FOV 1900 is a two-dimensional space boundedby X and Y dimensions. Although the LiDAR system can collect data pointsfrom the entirety of FOV 1900, certain regions of interest (ROI) mayhave higher precedence over other regions within FOV 1900 (e.g., such asundesired regions that occupy all space within FOV 1900 that is not aROI). FIG. 19 shows five different illustrative ROIs 1910-1914 toillustrate different regions within FOV 1900 that require additionaldata points than other regions within FOV 1900. For example, ROI 1210occupies an entire band of a fixed y-axis height across the x-axis ofFOV 1900. ROIs 1911 and 1912 show localized ROIs below ROI 1910, andROIs 1913 and 1914 show localized ROIs above ROI 1910. It should beunderstood that any number of ROIs may exist and that the ROIs canoccupy any portion of FOV 1900. ROI module 1864 may operate inconjunction with other modules to enable additional data points to becollected in the ROIs in a manner that does not disrupt the operation ofthe LiDAR system.

Referring back to FIG. 18 , skew angle module 1866 may be operative tocontrol variable skew angles in embodiments where the skew angle isadjustable. Beam angle module 1868 may control the beam angle of one ormore light beams. MFM control module 1870 can control the rotation speedof multi-facet mirror 1842. Rotation axis tilt module 1872 may controlthe tilt axis of polygon 1852. Controller 1860 can coordinate theoperation of each module to generate the desired point map.

FIGS. 20A and 20B shows an illustrative multi-facet mirror arrangementbeing used in LiDAR system 2000 according to an embodiment. LiDAR system2000 includes polygon 2010 that rotates around rotation axis 2015, motor2002, and multi-facet mirror 2020. Multi-facet mirror 2020 includesfacets 2021 and 2022 that are connected together via joint member 2030.Facet 2022 is connected to motor 2002. Facet 2021 is parallel withrotation axis 2025 and facet 2022 is parallel with rotation axis 2026.Motor 2002 is operative to oscillate facet 2022 about rotation axis2026. Joint member 2030 can translate rotational movement of motor 2002(via facet 2022) to oscillate facet 2021 along rotation axis 2025. Forexample, joint member 2030 may be a constant velocity type of joint oruniversal joint that translates rotation of facet 2022 to facet 2021.Thus, even though only one motor is being used to drive oscillation offacets 2021 and 2022, joint member 2030 is able to translate rotation ofmotor 2002 such that both facets rotate about their respective axes.Thus, use of a single motor (i.e., motor 2002) in combination with jointmember 2030 advantageously eliminates the redundant use of one motor perrotational axis. Four beams may be aimed at mirror 2020, with threebeams interacting with facet 2021 and one beam interacting with facet2022. The beam and mirror arrangement produces a point cloud that isrelatively dense in the forward portion of the FOV and relatively sparsein the side portion of the FOV. See FIGS. 21A and 21B, which showrespective point map and aperture color map that may be generated usingLiDAR system 2000.

It is believed that the disclosure set forth herein encompasses multipledistinct inventions with independent utility. While each of theseinventions has been disclosed in its preferred form, the specificembodiments thereof as disclosed and illustrated herein are not to beconsidered in a limiting sense as numerous variations are possible. Eachexample defines an embodiment disclosed in the foregoing disclosure, butany one example does not necessarily encompass all features orcombinations that may be eventually claimed. Where the descriptionrecites “a” or “a first” element or the equivalent thereof, suchdescription includes one or more such elements, neither requiring norexcluding two or more such elements. Further, ordinal indicators, suchas first, second or third, for identified elements are used todistinguish between the elements, and do not indicate a required orlimited number of such elements, and do not indicate a particularposition or order of such elements unless otherwise specifically stated.

Moreover, any processes described with respect to FIGS. 1-21 , as wellas any other aspects of the invention, may each be implemented bysoftware, but may also be implemented in hardware, firmware, or anycombination of software, hardware, and firmware. They each may also beembodied as machine- or computer-readable code recorded on a machine- orcomputer-readable medium. The computer-readable medium may be any datastorage device that can store data or instructions which can thereafterbe read by a computer system. Examples of the computer-readable mediummay include, but are not limited to, read-only memory, random-accessmemory, flash memory, CD-ROMs, DVDs, magnetic tape, and optical datastorage devices. The computer-readable medium can also be distributedover network-coupled computer systems so that the computer readable codeis stored and executed in a distributed fashion. For example, thecomputer-readable medium may be communicated from one electronicsubsystem or device to another electronic subsystem or device using anysuitable communications protocol. The computer-readable medium mayembody computer-readable code, instructions, data structures, programmodules, or other data in a modulated data signal, such as a carrierwave or other transport mechanism, and may include any informationdelivery media. A modulated data signal may be a signal that has one ormore of its characteristics set or changed in such a manner as to encodeinformation in the signal.

It is to be understood that any or each module or state machinediscussed herein may be provided as a software construct, firmwareconstruct, one or more hardware components, or a combination thereof.For example, any one or more of the state machines or modules may bedescribed in the general context of computer-executable instructions,such as program modules, that may be executed by one or more computersor other devices. Generally, a program module may include one or moreroutines, programs, objects, components, and/or data structures that mayperform one or more particular tasks or that may implement one or moreparticular abstract data types. It is also to be understood that thenumber, configuration, functionality, and interconnection of the modulesor state machines are merely illustrative, and that the number,configuration, functionality, and interconnection of existing modulesmay be modified or omitted, additional modules may be added, and theinterconnection of certain modules may be altered.

Whereas many alterations and modifications of the present invention willno doubt become apparent to a person of ordinary skill in the art afterhaving read the foregoing description, it is to be understood that theparticular embodiments shown and described by way of illustration are inno way intended to be considered limiting. Therefore, reference to thedetails of the preferred embodiments is not intended to limit theirscope.

What is claimed is:
 1. A light detection and ranging (LiDAR) system for use with a vehicle, comprising: a light source operative to emit one or more light beams; a multi-faceted polygon structure that is operative to control scanning the light beams in a horizontal direction of a field of view (FOV) of the LiDAR system, wherein an angle of at least one facet of the multi-faceted polygon structure with respect to a rotational axis of the multi-faceted polygon structure is a non-zero angle; a moveable mirror positioned to redirect the light beams passing between the light source and the multi-faceted polygon structure, the moveable mirror being operative to control scanning the light beams in a vertical direction of the FOV of the LiDAR system; and a skew angle controller operative to control a skew angle of the moveable mirror, wherein the skew angle of the moveable mirror is formed by a planar surface of the moveable mirror with respect to a rotational axis of the moveable mirror.
 2. The LiDAR system of claim 1, wherein the moveable mirror is operative to at least partly produce a point cloud that is dense in one predetermined portion and sparse in another predetermined portion.
 3. The LiDAR system of claim 2, wherein the light source is operative to emit a plurality of light beams, wherein the point cloud is at least partially produced using an arrangement of the plurality of light beams and the moveable mirror, the point cloud being dense in the forward portion of the FOV and sparse in the side portion of the FOV.
 4. The LiDAR system of claim 1, wherein the moveable mirror is a single facet mirror.
 5. The LiDAR system of claim 4, wherein a rotational axis of the single facet mirror is parallel to a planar face of the single facet mirror.
 6. The LiDAR system of claim 5, wherein the single facet mirror is positioned to direct two light beams to a same facet of the multi-faceted polygon structure.
 7. The LiDAR system of claim 5, wherein the single facet mirror is positioned to direct two light beams to two neighboring facets of the multi-faceted polygon structure.
 8. The LiDAR system of claim 1, further comprising: a detector configured to detect returned light pulses; and a lens configured to focus returned light pulses to the detector.
 9. The LiDAR system of claim 1, wherein the light source is a fiber optic light source.
 10. The LiDAR system of claim 1 wherein the light source is a semiconductor based emitter light source.
 11. The LiDAR system of claim 1, wherein the multi-faceted polygon structure is operative to rotate about a rotational axis at one or more predetermined speeds.
 12. The LiDAR system of claim 1, wherein a rotational axis of the multi-faceted polygon structure and a gravity axis of the multi-faceted polygon structure form a tilt angle.
 13. The LIDAR system of claim 1, wherein the multi-faceted polygon structure and the moveable mirror are positioned at different vertical heights. 